CA1004477A - Diverter valve for a gas turbine with an augmenter - Google Patents

Diverter valve for a gas turbine with an augmenter

Info

Publication number
CA1004477A
CA1004477A CA205,261A CA205261A CA1004477A CA 1004477 A CA1004477 A CA 1004477A CA 205261 A CA205261 A CA 205261A CA 1004477 A CA1004477 A CA 1004477A
Authority
CA
Canada
Prior art keywords
augmenter
gas turbine
diverter valve
diverter
valve
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
CA205,261A
Other versions
CA205261S (en
Inventor
Charles S. Lyons
Ronald C. Hollett
Dudley O. Nash
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
General Electric Co
Original Assignee
General Electric Co
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by General Electric Co filed Critical General Electric Co
Application granted granted Critical
Publication of CA1004477A publication Critical patent/CA1004477A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/56—Reversing jet main flow
    • F02K1/60—Reversing jet main flow by blocking the rearward discharge by means of pivoted eyelids or clamshells, e.g. target-type reversers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/56—Reversing jet main flow
    • F02K1/60—Reversing jet main flow by blocking the rearward discharge by means of pivoted eyelids or clamshells, e.g. target-type reversers
    • F02K1/605—Reversing jet main flow by blocking the rearward discharge by means of pivoted eyelids or clamshells, e.g. target-type reversers the aft end of the engine cowling being movable to uncover openings for the reversed flow
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/78—Other construction of jet pipes
    • F02K1/82—Jet pipe walls, e.g. liners
    • F02K1/822—Heat insulating structures or liners, cooling arrangements, e.g. post combustion liners; Infrared radiation suppressors
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00—Fluid handling
    • Y10T137/8593—Systems
    • Y10T137/877—With flow control means for branched passages
    • Y10T137/87788—With valve or movable deflector at junction
    • Y10T137/87812—Pivoted valve or deflector

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Exhaust Silencers (AREA)
CA205,261A 1973-11-21 1974-07-22 Diverter valve for a gas turbine with an augmenter Expired CA1004477A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US00417954A US3837411A (en) 1973-11-21 1973-11-21 Diverter valve for a gas turbine with an augmenter

Publications (1)

Publication Number Publication Date
CA1004477A true CA1004477A (en) 1977-02-01

Family

ID=23656036

Family Applications (1)

Application Number Title Priority Date Filing Date
CA205,261A Expired CA1004477A (en) 1973-11-21 1974-07-22 Diverter valve for a gas turbine with an augmenter

Country Status (2)

Country Link
US (1) US3837411A (en)
CA (1) CA1004477A (en)

Families Citing this family (32)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3943707A (en) * 1974-10-23 1976-03-16 General Electric Company Gas turbine engine exhaust nozzle diverter valve
US4000612A (en) * 1975-07-28 1977-01-04 General Electric Company Cooling system for a thrust vectoring gas turbine engine exhaust system
DE2540537C2 (en) * 1975-09-11 1977-11-10 Motoren- und Turbinen-Union München GmbH, 8000 München Gas turbine jet engine for propelling and controlling an aircraft
US4000854A (en) * 1975-10-02 1977-01-04 General Electric Company Thrust vectorable exhaust nozzle
US4529130A (en) * 1982-04-26 1985-07-16 Rolls-Royce Inc. Turbo machine nozzle with thrust reverser
GB2254589B (en) * 1983-12-20 1993-04-14 British Aerospace Jet propulsion powerplants
US4605169A (en) * 1983-12-27 1986-08-12 United Technologies Corporation Exhaust nozzle construction
US4753392A (en) * 1984-11-02 1988-06-28 United Technologies Corporation Two dimensional gas turbine engine exhaust nozzle
US4790495A (en) * 1984-12-06 1988-12-13 Grumman Aerospace Corporation Cascade thrust reverser
US4742961A (en) * 1987-05-04 1988-05-10 United Technologies Corporation Exhaust gas nozzle including a cooling air diverter
US4848081A (en) * 1988-05-31 1989-07-18 United Technologies Corporation Cooling means for augmentor liner
US4922711A (en) * 1988-06-10 1990-05-08 The Boeing Company Thrust reversing system for high bypass fan engines
DE3831062A1 (en) * 1988-09-13 1990-03-15 Stober & Morlock DEVICE BEHIND A GAS TURBINE
US5244014A (en) * 1989-05-23 1993-09-14 Henry Ehrenberg Multi-way valve
FR2651021B1 (en) * 1989-08-18 1994-05-06 Hispano Suiza Sa TURBOREACTOR DRIVE INVERTER, WITH DOORS ASSOCIATED WITH AN UPSTREAM PANEL
US5039171A (en) * 1989-08-18 1991-08-13 Societe Anonyme Dite Hispano-Suiza Multi-panel thrust reverser door
GB9127505D0 (en) * 1991-03-11 2013-12-25 Gen Electric Multi-hole film cooled afterburner combustor liner
NL9101782A (en) * 1991-10-24 1993-05-17 Philip Rijk Koudijs EXHAUST SYSTEM FOR COMBUSTION GASES.
DE4433759C1 (en) * 1994-09-22 1996-02-08 Mtu Muenchen Gmbh Jet engine with thrust reverser
US5706650A (en) * 1995-08-09 1998-01-13 United Technologies Corporation Vectoring nozzle using injected high pressure air
US5987880A (en) * 1997-07-08 1999-11-23 Mcdonnell Douglas Corporation Supersonic engine, multi-port thrust reversing system
US6938408B2 (en) * 2001-04-26 2005-09-06 Propulsion Vectoring, L.P. Thrust vectoring and variable exhaust area for jet engine nozzle
FR2834533B1 (en) * 2002-01-10 2004-10-29 Hurel Hispano Le Havre DEVICE FOR COOLING THE COMMON NOZZLE ON A NACELLE
US7871242B2 (en) * 2007-05-31 2011-01-18 United Technologies Corporation Single actuator controlled rotational flow balance system
US9157394B2 (en) 2012-08-15 2015-10-13 United Technologies Corporation Adjustable cable for exhaust duct liner hanger
US20160305370A1 (en) * 2015-04-16 2016-10-20 Honeywell International Inc. Translating cowl thrust reverser with door pivots aft of reverse flow path
CN104896514A (en) * 2015-05-13 2015-09-09 广东电网有限责任公司电力科学研究院 Anti-vibration heat insulation wall of main combustion chamber of gas turbine
US20170058828A1 (en) * 2015-08-26 2017-03-02 Rohr, Inc. Cascade with varying vane trailing edge thickness
US10563614B2 (en) * 2016-08-17 2020-02-18 Honeywell International Inc. Composite translating cowl assembly for a thrust reverser system
US10767596B2 (en) * 2017-07-26 2020-09-08 Raytheon Technologies Corporation Nacelle
US11046445B2 (en) 2017-07-26 2021-06-29 Raytheon Technologies Corporation Nacelle
US11891026B1 (en) * 2023-05-16 2024-02-06 King Faisal University Reverse thrust braking system

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2964905A (en) * 1960-12-20 Aircraft control means
GB1033583A (en) * 1965-03-17 1966-06-22 Rolls Royce Thrust reverser for a jet propulsion engine
BE755612A (en) * 1969-06-18 1971-02-15 Gen Electric PROPULSION TUBES WITH IMPROVED NOISE CANCELLATION SYSTEM
US3614037A (en) * 1969-09-22 1971-10-19 Boeing Co Aircraft combination thrust reverser and sound suppressor and a particular full range balanced thrust reverser
DE1964976C3 (en) * 1969-12-24 1973-01-04 Motoren- Und Turbinen-Union Muenchen Gmbh, 8000 Muenchen Thrust reverser for a turbine jet engine of an aircraft
US3690561A (en) * 1970-11-05 1972-09-12 Rohr Corp Thrust controlling system
US3690562A (en) * 1971-06-23 1972-09-12 Gen Motors Corp Jet propulsion nozzle

Also Published As

Publication number Publication date
US3837411A (en) 1974-09-24

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